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Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation

By Jan Navrátil

Abstract

Thesis summarizes conceptual design of VUT 001 Marabu airplane modification to fulfill CS-22 regulation requirements. Aerodynamical optimalization of wing and horizontal tail geometry is solved. Aerodynamical characteristics, performance and stability is analysed and basic structural design of wing and horizontal tail is performed

Topics: Marabu; VUT 001; Conceptual design; CS-22; Koncepční návrh
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
Year: 2008
OAI identifier: oai:invenio.nusl.cz:228059
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